View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 19120U 26020.14956323 +.00000000 +00000-0 +96843-4 0 00003
2 19120 71.0140 171.1845 0020004 50.5653 309.7238 14.19607678 06
| Epoch (UTC): | 20 January 2026 03:35:22 |
| Eccentricity: | 0.0020004 |
| inclination: | 71.0140° |
| perigee height: | 812 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 171.1845° |
| argument of perigee: | 50.5653° |
| revolutions per day: | 14.19607678 |
| mean anomaly at epoch: | 309.7238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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